Douglas DC-9-31

Service difficulty reports · 7,433

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR GTIA9700128Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD RIGHT SIDE, 1ST 2ND, 3RD HORIZONTAL BULKHEAD FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILLED CRACKS, FABRICATED DOUBLERS AND INSTALL IAW 53-01 FIG 2. (M)Dec 9, 1996 · N928ML · Doug DC931 · Fuselage Main, BulkheadSDR GTIA9700127Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD RT SIDE 4TH HORIZONTAL BULKHEAD FRAME UP FROM CABIN FLOOR PANEL IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, FABRICATED DOUBLERS AND INSTALLED IAW 51-10-2, 51-10-3, 53-01 FIG 2. (M)Dec 9, 1996 · N928ML · Doug DC931 · Fuselage Main, BulkheadSDR GTIA9700045Floor Panel · crackedMHV - FLOOR PANEL NR 10 FORWARD HAS 3 HAT SECTIONS WITH CRACKS IN CORNERS (2 AT 1 END AND ONE AT THE OTHER END). ALSO, INSULATION BATTING FALLING APART. REPAIRED HAT SECTIONS IAW SRM 53-05, ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED INSULATION PER MM 25-Dec 9, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700044Door · crackedMHV - PASSENGER ENTRY DOOR NUMEROUS CRACKS. REPAIR DOOR IAW 52-05, 51-30-2, 51-30-5. (M)Dec 9, 1996 · N928ML · Doug DC931 · Passenger/Crew DoorsSDR 9626209975T-Duct · failedDURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTEND LIGHT. AIRCRAFT APPEARED TO ROLL SLIGHTLY TO THE LEFT. CREW EXECUTED GO-AROUND PROCEDURES, AN UNEVENTFUL LANDING WAS ACCOMPLISHED WITH FLAPS AT 40 DEGREES AND NO SLATS. MAINTENANCDec 9, 1996 · N9339 · Doug DC931 · Leading Edge Slat Control SystemSDR 961211001Windshield · failedDTW - FLT 634 - IN CRUISE CONFIGURATION, OBSERVED ARCING FOLLOWED BY A LARGE FLASH IN THE CAPTAIN'S WINDSHIELD. CAPTAIN'S WINDSHIELD CIRCUIT BREAKER'S TRIPPED. CORRECTIVE ACTION: MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD AND WINDSHIELD TEMP Dec 9, 1996 · N969ML · Doug DC931 · Flight Compartment WindowsSDR GTIA9700126Frame · corrodedMHV - SURFACE CORROSION ON FORWARD SIDE OF FRAME 1ST IN FRONT OF AFT PIT AFT BULKHEAD BETWEEN LONGERON 30 AND 29. FABRICATED NEW SECTION OF RIB AND FILLER. REMOVED CORROSION OFF OF FRAME THAT WAS WITHIN LIMITS. REMOVED 2.70 BY 80 SECTION OF FRAME THAT WAS ODec 8, 1996 · N928ML · Doug DC931 · Fuselage Main, FrameSDR 9626199991Sidewall Lights · smokingEN ROUTE, PASSENGER REPORTED SMOKE COMING FROM SIDEWALL LIGHTS AT ROW 9 ON LEFT SIDE. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED SIDEWALL LIGHTS PER MEL 33-2. SUSPECT BAD BALLAST.Dec 8, 1996 · N8957E · Doug DC931 · Passenger Compartment LightingSDR 9626189990Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES.Dec 8, 1996 · N8950E · Doug DC931 · Emergency LightingSDR 9626169969Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS AT ROW 11 VERY WEAK. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Dec 8, 1996 · N9333 · Doug DC931 · Emergency LightingSDR GTIA9700125Stringer · corrodedMHV - NUMEROUS PATCHES OF SURFACE CORROSION ALONG TOP OF RIGHT STRINGER FORWARD OF AFT CARGO DOOR TO FORWARD BULKHEAD OF AFT PIT. SECTION CLOSEST TO CARGO DOR IS DELAMINATING. REMOVED BOTH ENDS, FABRICATED AND INSTALLED (2) SPLICES AND (2) ENDS IAW SRM 53-02Dec 7, 1996 · N928ML · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9626239952Longeron · crackedDURING PERIODIC CHECK, FOUND LONGERON 30 'T' CHORD CRACKED IN RADIUS AT FS 609, RIGHT KEEL AREA. REPAIRED PER EA 99-120157.Dec 7, 1996 · N916RW · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9626179981Battery Pack · dischargedDURING PERIODIC CHECK, THE RIGHT NACELLE EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Dec 7, 1996 · N994Z · Doug DC931 · Emergency LightingSDR 9626149981Slide · low batteryDURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.Dec 7, 1996 · N994Z · Doug DC931 · Escape SlideSDR 961209002Retract Mech · lack of lubeBUF - FLT 856 - IN CLIMB CONFIGURATION WHEN LANDING GEAR RETRACTED, A LOUD FLUCTUATING SOUND WAS PRODUCED. SOUNDED LIKE NOSE LANDING GEAR DOORS. CORRECTIVE ACTION: MAINTENANCE INSPECTED NOSE LANDING GEAR DOORS, FOUND NOT TO BE SECURED. LUBRICATED NOSE GEAR Dec 7, 1996 · N934ML · Doug DC931 · Landing Gear Door Retract SectionSDR USAA960777Angle · corrodedPIT - DURING Q-1, C-2 CHECK, FOUND SKIN BULGE AT CUSP ANGLE AT STATION 996, LONGERON 18R. SPLICED IN NEW SECTION OF CUSP ANGLE PER SRM 53-05 FIG 25. CORROSION TASK NR C50-53300, CORROSION LEVEL 1. (M)Dec 6, 1996 · N933VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA970041Floor Panel · damagedMHV - COCKPIT FLOOR AT STATION 117 RBL 3 INCH FROM CENTER LINE EXISTS DENTS AND A CRACK .823 INCH LONG THROUGH SUB STRUCTURE BARRIER FLOOR AND PLASTIC CABLE SHROUD. REMOVED DAMAGED AREA, FABRICATED AND INSTALL DOUBLERS PER SRM 53-01 FIG 2, 51-10-03, 51-30-02,Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700124Air Stair · mis repairedMHV - PERFORM REPAIR PER DOUGLAS SERVICE REWORK DRAWING SR09530219 (STAIR DOOR AREA). REMOVED TEMP REPAIR, FABRICATED NEW DOUBLERS AND FILLER IAW SRM 53-05-17A. INSTALLED PER DRAWINGS SR09530031 AND SR09530219. (M)Dec 6, 1996 · N928ML · Doug DC931 · Entrance StairsSDR GTIA9700119Frame · corrodedMHV - FRAME HAS CORROSION AT STATION 945 RBL 61 AND 63 AF1 AND 3. FABRICATED AND INSTALLED NEW WEB IAW 51-10-2 AND 51-30-0. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Main, FrameSDR GTIA9700118Floor · corrodedMHV - FLOOR WEB HAS CORROSION AT STATION 902 RBL 59 ZF1 AND STATION 908 RBL 59 HAS EVIDENCE OF CORROSION BETWEEN WEBS. FABRICATED AND REPLACED CORRODED WEB IAW 51-10-3/51-30-0. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700113Angle · corrodedMHV - FORWARD ACC COMP, FLOOR SUPPORT ANGLE AT FS STATION 217 HAS SEVERAL CORRODED CLIPNUTS AND LIGHT CORROSION ON BOTTOM SIDE. REMOVED AND REPLACED ANGLE AND CLIPNUTS IAW SRM 51-30-2, 51-30-8. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700043Floor Panel · damagedNR 30 FLOOR PANEL HAS 3 CRACKS. REMOVED DAMAGED MATERIAL, DOT LOCATION 24, 25, 26 AND FABRICATED FILLERS AND DOUBLERS. ALODINED AND PRIMED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED RIVETS PER SRM 51-30-3. REPAIRED PER SRM 53-05, Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700042Floor Panel · damagedMHV - COCKPIT FLOOR AT STATION 142 RBL 17 INCH FROM CENTERLINE EXISTS A HOLE .275 INCH DIAMETER THROUGH SUB STRUCTURE BARRIER FLOOR. REMOVED DAMAGE AREA AND FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-01 FIG 2, 51-30-02. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700040Floor Panel · crackedMHV - FLOOR PANEL NR 2A HAS SEVERAL SMALL CRACKS AT THE END ROW OF RIVET HOLES. STOP DRILLED HOLE AND ADDED DOUBLER IAW 51-10-3, SRM 51-10-4. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700039Floor · corrodedMHV - FLOOR WEB HAS CORROSION ON STATION 931-948 RBL 59 ZF1. REMOVED DAMAGE, FABRICATED NEW WEB AND INSTALLED IAW 51-10-2, 51-10-3, 51-30-0. (M)Dec 6, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR 9626229945Frame · elongated holeDURING PERIODIC CHECK, FOUND FRAME AT FS 1038 BETWEEN LONGERONS 13L AND 14L WITH AN ELONGATED HOLE FROM BRACE ROD ATTACH FITTING. REPAIRED FRAME PER EA 99-111-14.Dec 6, 1996 · N8925E · Doug DC931 · Fuselage Main, FrameSDR USAAD96177Charger · failedIND - AFTER EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, REPAIRED WIRING IN SECTIONS 3 AND 4. (M)Dec 5, 1996 · N943VJ · Doug DC931 · Emergency LightingSDR GTIA9700116Angle · corrodedMHV - FLOOR SUPPORT REPAIR HAS CORROSION AT STATION 218 BL 0 ZF-1 AND STATION 237 BL 0 ZF-1. REMOVED AND REPLACED CORRODED ANGLES, NEW ANGLES WERE FABRICATED AND INSTALLED IAW 51-30-2, 51-10-3, 51-10-4, 51-30-0, AND 53-03 FIG 3. (M)Dec 5, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9615001Power Supply · failedSTL - FLT 517 - DURING CRUISE, EGRESS LIGHTS ILLUMINATED AT SEAT ROWS 1 TO 7. FOUND FAULTY POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C - 11-13-95 - STL.Dec 4, 1996 · N982PS · Doug DC931 · Emergency LightingSDR GTIA9700038Structure · damagedMHV - FLOORBOARD 27, 3 HAT SECTIONS CRACKED AT ONE END AND 2 SECTIONS CRACKED AT OTHER END. INSULATION BATTING MISSING ON ONE END, FALLING APART ON THE OTHER, AND UNBONDED AND FALLING APART AT A FEW AREAS IN THE CENTER SECTION. REMOVED 5 CRACKED HAT SECTIONSDec 4, 1996 · N928ML · Doug DC931 · Fuselage Main, StructureSDR 9626019905Bolt · misinstalledRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT STAYED ON. MAINTENANCE FOUND BOLT HEAD ON ROLLER AND LINK ASSEMBLY HITTING ON FORWARD EDGE OF RIGHT WHEEL WELL APPROXIMATELY 1.5 INCHES ABOVE DOOR SWITCH. REMOVEDec 4, 1996 · N955N · Doug DC931 · Landing Gear Door Retract SectionSDR 9625979978Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK OK.Dec 4, 1996 · N9342 · Doug DC931 · Emergency LightingSDR 9625939952Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON BELLY SKIN FROM FS 529 TO FS 584, LONGERONS 26L TO 26R. INSTALLED REPLACEMENT SKIN PER EA 99-120159. L/P 0899331.Dec 4, 1996 · N916RW · Doug DC931 · Fuselage Main, Plate/SkinSDR 9625929952Frame · crackedDURING PERIODIC CHECK, FOUND LOWER FLANGE OF FUSELAGE FRAME CRACKED FS 598, LONGERON 30L. REPAIRED PER EA 99-120158. L/P 0899286.Dec 4, 1996 · N916RW · Doug DC931 · Fuselage Main, FrameSDR 9625919914Press Panel · crackedDURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED APPROXIMATELY 2 INCHES AT RIGHT SIDE FRAME ATTACH POINT, F.S. 83. REPAIRED PER EA 99-111235. L/P 0899335.Dec 4, 1996 · N964N · Doug DC931 · Fuselage Miscellaneous StructureSDR 9625909980Skin · corrodedDURING PERIODIC CHECK, FOUND SKIN AT RIGHT KEEL CORRODED BETWEEN FS 676 AND FS 698. REPLACED SKIN AND INSTALLED DOUBLER AND SHIMS PER EA 99-111913. L/P 0899472.Dec 4, 1996 · N9344 · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD96175Charger · failedMID CABIN FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE IN CHARGER ASSEMBLY OPEN AND CORRODED. REPLACED CHARGER ASSEMBLY. (M)Dec 3, 1996 · N976VJ · Doug DC931 · Emergency LightingSDR GTIA9700037Floor Panel · crackedMHV - FLOOR PANEL AFT CABIN HAS TWO CRACKS IN AFT AREA OF SKIN. CUT OUT CRACKS AND FABRICATED FILLER AND DOUBLER PER SRM 51-10-2. ALODINED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED FASTENERS PER SRM 51-30-2. FLOOR PANEL REPAIR CODec 3, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700036Jamb · damagedMHV - AFT CARGO PIT, LOWER FORWARD CORNER OF DOOR JAMB HAS DAMAGE ON EDGE OF DOUBLER AND IS DELAMINATING AND HAS NUMEROUS DAMAGED FASTENERS. FABRICATED DOUBLER AND INSTALLED WITH SRM 51-10-2 AND 51-10-3. (M)Dec 3, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700035Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD DOOR CANTED FRAME ON RT SIDE OF DOOR FRAME IS CRACKED AT UPPER END WHERE THE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED FRAME, TRIM CRACK AREA PER SRM 51-01, DYE PEN, NO CRACKS FOUND. REINSTALLED FRAME IAW SRM 51-10-3, 53-11-3 PAGEDec 3, 1996 · N928ML · Doug DC931 · Fuselage Main, BulkheadSDR GTIA9700034Channel · crackedMHV - LEFT OUTBOARD GEAR DOOR U-CHANNEL AT AFT SURFACE OF DOOR IS CRACKED. REMOVED OLD PART FABRICATED AND INSTALLED NEW PART IAW 52-10-2, 52-80-0. (M)Dec 3, 1996 · N928ML · Doug DC931 · Landing Gear DoorsSDR 9625959980Pressure Panel · crackedDURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED AT FS 83, LEFT AND RIGHT SIDE. REPAIRED PER EA 99-111904. L/P 0899110, 0899101.Dec 3, 1996 · N9344 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9625949980Pressure Panel · crackedDURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED AT FS 110, LEFT AND RIGHT AT INBOARD AND OUTBOARD TOP VERTICAL SUPPORT. REPAIRED PER EA 99-111906. L/P 0898978, 0898972, 0898965.Dec 3, 1996 · N9344 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9625859906O-Ring · brokenFUEL LEAKING FROM LEFT WING AFTER TAKEOFF. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAK AT DUCT CONNECTION BETWEEN CROSSFEED VALVE AND FORWARD RIGHT FUEL PUMP. REPLACED O-RINGS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO Dec 3, 1996 · N956N · Doug DC931 · Aircraft Fuel Distribution SystemSDR 9625829967Connector · not seatedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 14 AND 17 INOPERATIVE. MAINTENANCE RESEATED CONNECTION AT ROW 14. OPERATIONAL CHECK NORMAL.Dec 3, 1996 · N9331 · Doug DC931 · Emergency LightingSDR 9625789991Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM CLIPS. MAINTENANCE ADJUSTED CLIPS. OPERATIONAL CHECK NORMAL.Dec 3, 1996 · N8957E · Doug DC931 · Aerodynamic FairingsSDR USAAD96176Comm Syst · malfunctionedFLT 2048 - SWF-CLT - LOST BOTH COMM'S ON TAKEOFF. RETURNED TO FIELD. EVENTUALLY WERE ABLE TO TRANSMIT ON NUMBER 2, AND RECIEVE ON NUMBER 1. RERACKED NUMBER 1 AND 2 COMMS. FOUND NUMBER 1 LOOSE. SECURED BOTH. ALL CHECKED GOOD. (M)Dec 2, 1996 · N963VJ · Doug DC931 · VHF Communications SystemSDR GTIA9700033Brackets · crackedMHV - RIGHT WING LEADING EDGE WING STATION XRS 250 AND XRS 256 HAVE CRACKED MOUNTS. REMOVED OLD BRACKETS, FABRICATED IAW 51-10-2 AND INSTALLED IAW 51-10-1/3. (M)Dec 2, 1996 · N928ML · Doug DC931 · Wing Miscellaneous StructureSDR GTIA9700032Membrane · crackedMHV - CRACK IN MEMBRANE AT FS 950 48 INCHES LEFT OF A/C C/T. FABRICATED AND INSTALLED DOUBLERS IAW 53-01, PAGE 17, 51-10-3. (M)Dec 2, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700031Tie Clip · crackedMHV - PYLON SHEAR WEB TO LONGERON 17R, TIE CLIP IS CRACKED IN TWO, STATION 965. REPLACED TIE CLIP PER SRM 51-10-1, 51-10-3, 51-30-2. (M)Dec 2, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous Structure
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